Airframe Structural Components: 37W26021-4, 37W41068-2, 37W43119-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 37W26021-4 37W260214 | 1560-00-532-1262 | Fairing, Aircraft | Aircraft Mission Design Series: F-84 | Northrop Grumman Systems Corporation (26512) | |
| 37W32115-1 37W321151 | 1560-00-567-0862 | Collar, Aileron Cont | General Characteristics Item Description: Steel, 1.819 in. min, 1.820 max id, 2.061 in. od 1 end, 4.000 in. dia flange opposite end, 4.065 in. lg | Northrop Grumman Systems Corporation (26512) | |
| 37W32138-1 37W321381 | 1560-00-506-7129 | Block, Wing Root Ai | General Characteristics Item Description: Steel, MIL-S-18729, 2.360 in. lg, 1.240 in. W, 0.620 in. thk, 2 holes 0.313 in. dia, 1 hole 0.438 in. dia | Northrop Grumman Systems Corporation (26512) | |
| 37W38014-2 37W380142 | 1560-00-567-0888 | Fairlead Assembly, m | III End Item Identification: Aircraft model F84 General Characteristics Item Description: Steel | Northrop Grumman Systems Corporation (26512) | |
| 37W38139-1 37W381391 | 1560-00-628-1763 | Block, Main Landing Gear Door | General Characteristics Item Description: Steel, MIL-S-18729, 1.745 in. lg, 0.680 in. W, 0.620 in. thk, 0.437 in. dia hole thru side, 0.313 in. dia hole thru length | Northrop Grumman Systems Corporation (26512) | |
| 37W38297-11 37W3829711 | 1560-00-570-4803 | Striker, Uplock Sequ | General Characteristics Item Description: Steel, MIL-S-6758, comp 4130, cond D, forging size, 0.900 in. thk, 1.700 in. W, 2.860 in. lg | Northrop Grumman Systems Corporation (26512) | |
| 37W39351-3 37W393513 | 1560-00-620-2622 | Block, Actuator | General Characteristics Item Description: Steel, MIL-S-6758, 0.990 in. lg, 0.750 in. W, 0.310 in. thk | Northrop Grumman Systems Corporation (26512) | |
| 37W39352-1 37W393521 | 1560-00-532-1267 | Pin, Spoiler Pivot | General Characteristics Item Description: Steel, MIL-S-6758, 0.498 in. min, 0.499 max dia, 1.320 in. O/a LG0.386 in. hole drilled thru 0.660 in. from end, 0.070 in. dia groove 0.380IN. from both ends | Northrop Grumman Systems Corporation (26512) | |
| 37W41068-1 37W410681 | 1560-00-564-5162 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-84 Special Features: T shaped, 2 mntg holes 0.166 in dia countersunk 100 degrees by 0.279 in dia, 2 slots 0.344 in lg by 0.094 in W Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512) | |
| 37W41068-2 37W410682 | 1560-00-564-5164 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-84 Special Features: T shaped, 2 mntg holes 0.166 in dia countersunk 100 degrees by 0.279 in dia, 2 slots 0.344 in lg by 0.094 in W Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512) | |
| 37W41088-1 37W410881 | 1560-00-564-5209 | Arm Assembly, Uplock | General Characteristics Item Description: Steel, MIL-S-18729 | Northrop Grumman Systems Corporation (26512) | |
| 37W41112-3 37W411123 | 1560-00-713-7593 | Nut Assembly, Mlg Downstop | General Characteristics Item Description: Steel with 2 nylon plugs, 2.280 in. lg, 0.560 in. O/a dia, 1 hole 0.180 in. dia thru head, 2 holes thru shaft tap 10-32NF-3A MIL-S-7742, csk 100 deg X 0.190 in. dia both ends | Northrop Grumman Systems Corporation (26512) | |
| 37W41114-3 37W411143 | 1560-00-507-0120 | Pad, Upstop Landing Gear | General Characteristics Item Description: Synthetic rubber, MIL-R-6855, 2.500 in. thk, 0.760 in. W, 1.086 in. O/alg, 2 holes in line 0.219 in. dia, 0.326 apart | Northrop Grumman Systems Corporation (26512) | |
| 37W43042-1 37W430421 | 1560-00-564-5243 | Fork and Roller, Doo | III End Item Identification: Aircraft model F84 | Northrop Grumman Systems Corporation (26512) | |
| 37W43066-1 37W430661 | 1560-00-564-5261 | Stop Assembly, Door | III End Item Identification: Acft model RF84F General Characteristics Item Description: C/O bracket 1 ea P/N 37W43105-11C, spring 1 ea 37W43065-1, used on main landing gear outboard door linkage | Northrop Grumman Systems Corporation (26512) | |
| 37W43066-2 37W430662 | 1560-00-564-5263 | Stop Assembly | III End Item Identification: Aircraft model F84 | Northrop Grumman Systems Corporation (26512) | |
| 37W43070-38 37W4307038 | 1560-00-339-9502 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-84 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
| 37W43070-67 37W4307067 | 1560-00-614-2688 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-84 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
| 37W43106-2-1 37W4310621 | 1560-00-564-5291 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5, T3 fed spec single material response Securing Device Type: Turnlock fastener | Northrop Grumman Systems Corporation (26512) | |
| 37W43119-1 37W431191 | 1560-00-612-3513 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-84 Aircraft Location: Landing gear door uplock Overall Length: 1.880 inches nominal | Northrop Grumman Systems Corporation (26512) |